JASC 2750
Service difficulty reports · 10,201
Reports filed under 2750 · Trailing Edge Flap Control System, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2750' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2750' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR F3LA00116Carriage · corrodedDEN - FOUND DURING C-7 CHECK INSPECTION, FOUND PITTING CORROSION ON LT INBOARD MID-FLAP OUTBOARD CARRIAGE ON INSIDE DIAMETER OF TORQUE TUBE HOLES. MAINTENANCE REPLACED LT INBOARD MID FLAP OUTBOARD CARRIAGE ASSY. (M)SDR USAASB00153Flap · jammedTPA - FLT 2797 - AS AIRCRAFT WAS BEING CONFIGURED FOR FINAL APPROACH TO TPA, THE RIGHT INBOARD TRAILING EDGE FLAP BECAME JAMMED WHEN THEY WERE MOVED FROM 10-15 DEGREES. CREW ACCOMPLISHED PROCEDURES AND A GO-AROUND AND DECLARED AN EMERGENCY. FLIGHT LANDED WITSDR AU000440Controller · faulty(AUS) FLAPS FAULTY. FLAPS CHECKED ON GROUND AND OPERATED WITHOUT FAULT.SDR COMA0060466Power Unit · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FLAP POWER DRIVE UNIT.SDR LR7A0053Jackscrew · wornDURING APPROACH FOR LANDING AT WSAP FLAPS STOPPED AT 60% DURING EXTENSION. CONTINUED APPROACH AND LANDED WITHOUT INCIDENT.DURING SCHEDULED B1 CHECK ACCOMPLISHED VISUAL INSPECTION OF ALL FLAP TORQUE SHAFT CONNECTIONS AND ASYMETRIC BRAKE ASSY. NO DEFECTS NOTEDSDR COMA0060461Bpsu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND BPSU.SDR VNAA0005011Control Box · failedDURING TAKEOFF THE CREW RECEIVED A FLAP CONTROL FAIL CAS MESSAGE. THE CREW THEN ABORTED TAKEOFF. MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL BOX IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-50-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT SDR COMA0060460Fcu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FECU.SDR COMA0060459Warning System · activatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0060458Bpsu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND BPSU.SDR DL72S001028Flap Track · corrodedINBOARD FLAP, NR 5 INBOARD TRACK CORROSION FOUND ON MLG BEAM ATTACH BOLT HOLES AND SPOTFACES, THE SPACER BAR ATTACH BOLT HOLE, AND THE TOGGLE DETENT HOLE. REPAIR PER ER/A 387640-14AD AND BFGOOFRICH ENGINEERING REPAIR NR 23-0801.SDR COMA0060450Warning System · failedFLAPS FAILED AT 26 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0060449Ecu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FECU.SDR ASOA00059Power Unit · inoperativeFLT 4444 - ON DOWNWIND FOR RUNWAY 22 AT 210 KTS, CREW SELECTED FLAPS TO 8 DEGREES AND FLAPS FAIL MESSAGE APPEARED ON EICAS. CREW FOLLOWED PROCEDURES AS LAID OUT IN ABNORMAL SECTION OF QRH PAGE 8-8. CREW INFORMED ATC OF SITUATION, DECLARED AN EMERGENCY, AND RSDR QXEA0001583Universal Joint · wornYYC- LEFT HAND WHEEL BAY FLAP DRIVE TUBE U JOINT IS WORN. REPAIRED IAW FOKKER SRM 27-51-04.SDR COMA0060447Warning Light · illuminatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0060441Flap · malfunctionedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR ASOA00062Connector · inoperativeFLT 4538 - CLIMBING THROUGH 21,000 FEET, CREW RECEIVED A FLAP FAIL MESSAGE. CREW PERFORMED FLAPS FAIL PROCEDURE AND CALLED ATL FLIGHT CONTROL. CREW THEN DECLARED AN EMERGENCY AND RETURNED TO ATL. CAPTAIN SAFELY PERFORMED A ZERO DEGREE FLAP LANDING. MAINTENSDR 20000608SH013Housing · contaminatedUNIT WAS NOTED TO BE ROUGH IN OPERATION CAUSED FROM CONTAMINATED MIL-H-5606 FLUID. THE NON-STANDARD SLEEVE REPAIR TO HOUSING, COMMON TO THE BORE FORE BEARING, WAS FOUND ROTATING IN THE HOUSING. THIS CAUSED THE FLUID TO BECOME CONTAMINATED WITH ALUMINUM. (X)SDR QXEA0001359Flap Track · corrodedPDX- RIGHT HAND WING NR 1 FLAP TRACK TOP SURFACE OF THE LOWER RAIL HAS SURFACE CORROSION. REPAIRED IAW RD 8-57-985.SDR CA000530074Wire · chafed(CAN) DURING CLIMB, THE FLAP CONTROL CIRCUIT BREAKER TRIPPED AS THE FLAPS WERE BEING RETRACTED. THE BREAKER WAS RESET AND IT TRIPPED AGAIN. THE FLIGHT WAS CONTINUED WITH THE FLAPS PARTIALLY EXTENDED. MAINTENANCE PERSONNEL FOUND THE FLAP CONTROL CIRCUIT WIRINSDR QXEA0001357Flap Track · corrodedPDX- LEFT HAND FLAP TRACK OUTBOARD VERTICAL, SMALL PIT ON FORWARD SECTION OF TRACK. REPAIRED IAW RD 8-57-1168.SDR QXEA0001356Flap Track · corrodedPDX- LEFT HAND FLAP TRACK OUTBOARD VERTICAL, SMALL PIT ON FORWARD SECTION OF TRACK. REPAIRED IAW RD 8-57-1167.SDR TSAA0027136Transmitter · malfunctionedFLT 91 - OGG-HNL - DURING TAKEOFF FROM OGG, THE STALL WARNING STICK SHAKER BEGAN AT ROTATION AND WAS CONTINUOUS THROUGH 1000 FEET AND INTERMITTENT AFTER THAT. RETURNED TO OGG FOR AN UNEVENTFUL LANDING. REPLACED THE RIGHT TRAILING EDGE FLAP POSITION TRANSMITTSDR AU000415Wire Rope · worn(AUS) FLAP SECONDARY DRIVE OUTER CABLE SWAGED COUPLING FLANGE WORNEXCESSIVELY.SDR GAIA00278Switch · inoperativeDEN/OAK - FLT 2026 - AFTER FLAP RETRACTION, THE NR 2 LEADING EDGE DEVICE DID NOT INDICATE RETRACTED. AMBER LIGHT REMAINED ON. THE CREW RETURNED TO DEN AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLACED LEADING EDGE FLAP POSITION SWITCH AND OPSDR COMA0060420Fcu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FECU.SDR 00FDEA00328Flap · stuckDURING NORMAL FLAPS EXT AT SLC, FLAPS STUCK IN FULL UP POSTION. SYS 1 & 2 FLAP FAULT LIGHT ON.SDR COMA0060407Flap · failedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR CA000505029Actuator · seized(CAN) DURING FINAL APPROACH A/C HAD FLAP FAILURE AT 40 DEGREES.SDR COMA0060408Flap · failedON APPROACH TO LANDING, FLAP FAIL AT 30 DER TIME 12:00 EST. DEFERRED FLAP FOR RE-INSPECT PER AD 98-20-01.SDR CA000530067Bpsu · failed(CAN) FLAPS FAILED AT 42 DEG ON APPROACH. BITE CHECK CARRIED OUT. RT BPSU REPLACED.SDR CA000530066Control Unit · failed(CAN) FLAP FAILED, FAULT CLEARED WITH A JOB CARD TO DO A VERIFICATION CHECK OF SYSTEM WAS ISSUED. FECU REPLACED. RIG CHECK CARRIED OUT.SDR COMA0060398Actuator · seizedFLAPS FAILED AT 40 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP, INBOARD ACTUATOR.SDR DL72L000869Switch · failedA/C AIR TURNBACK WITH PR. NR 6 KRUEGER FLAP FAILED TO RETRACT AFTER DEPARTURE. OPERATED FLAPS SEVERAL TIMES, FOUND NR 6 KRUEGER AND ALL FLAPS OPERATE NORMAL. FOUND L/E FLAP INTRANSIT AMBER LIGHT ON FWD PNL AND ON S/O''S PNL ILLUM. REPLACED THE NR 6 KRUEGERSDR JBXA0000173Bpsu · failedFLAPS FAILS AT 30 DEGREES ON APPROACH FLAPS FAIL MESSAGE ON EICAS INTO IND. FERRIED TO RDU. REPLACED RT BPSU. RIGGED FLAPS IAW CRJ 27-51-10, OPS CHECK GOOD.SDR UPS00232596Support Fitting · corrodedINSPECTION TYPE:C+SI, NR 5 FLAP TRACK FWD SUPPORT FITTING CORRODED. NR 5 FLAP TRACK FWD SUPPORT FITTING REPLACED IAW MM 20-80-01 & DRAWING NR 65-21651.SDR COMA0060393Flap · malfunctionedFLAPS AT 20, FLAPS NOT IN MOTION, FLAPS FAIL MSG, 11;45 EST. COMPLIED WITH EO 27-045AD, INSPECTION OF FLAPS, AND RESET OF SYSTEM. DEFERRED PER GMM 4-3 CAT 1 AND AD 98-20-01.SDR UPS00232597Support Fitting · corrodedINSPECTION TYPE:C+SI, NR 4 FLAP TRACK FWD SUPPPORT FITTING CORRODED. NR 4 FLAP TRACK FWD SUPPORT FITTING REPLACED IAW MM 20-80-01 & DRAWING 65-21651.SDR COMA0060387Warning System · activatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0060386Warning System · activatedFLAPS FAILED AT 8 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR MWEA00394Transmitter · inoperativeSTALL WARNING INDICATION FAILURE LIGHT ILLUMINATED CLIMBING THROUGH 25000 FEET AND RE-ILLUMINATED 2 MINUTES AFTER STALL WARNING TEST ON BOTH SYSTEMS. MAINTENANCE REMOVED AND REPLACED FLAP TRANSMITTER AND INDICATOR.SDR UPS00232614Flap Track · corrodedINSPECTION TYPE:C+SI, SURFACE CORROSION AT AFT O/B ATTACH HOLE FOR NR 5 FLAP TRACK ON RT ML G BEAM. REPAIRED IAW SMRO EO 2000-015-007 UPS ENGINEERING FILE NR 727-57-2154.SDR UPS00232613Flap Track · corrodedINSPECTION TYPE:C+SI, SURFACE CORROSION AT AFT O/B ATTACH HOLE FOR NR 4 FLAP TRACK ON LT ML B BEAM. REPAIR CARRIED OUT IAW SMRO EO 2000-015-006 UPS ENGINEERING FILE NR 727-57-2153.SDR COMA0060382Warning System · activatedFLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0060372Flap · out of rigFLAPS FAILED AT 30 DEGREES. ADJUSTED FLAP RIGGING, SYSTEM OPERATION NORMAL.SDR UPS00232612Flap Track · corrodedINSPECTION TYPE:C+SI, NR 6 FLAP TRACK AFT MOUNT OUTER SURFACE CORRODED (UPPER.) FOR REPAIR REF SMRO EO 2000-015-009 UPS ENGINEERING FILE NR 727-57-2152.SDR UPS00232611Flap Track · corrodedINSPECTION TYPE:C+SI, NR 3 FLAP TRACK CORROSION AT AFT MOUNT OUT SURFACE FOR REPAIR REF SMRO EO 2000-015-08 UPS ENGINEERING FILE NR 727-57-2151.SDR COMA0060380Pin · missingCONNECTING ROD, LEFT HAND OUTBOARD FLAP, IS NOT ATTACHED. REPLACED BUTE DOOR ACTUATOR ROD PIN.SDR UPS00232586Carriage · corrodedINSPECTION TYPE:C+SI, NR 2 FLAP CARRIAGE CORROSION AT SPINDLE INNER BORE AND SMALL BEARING OUTER SURFACE END. CARRIAGE ASSY REPLACED IAW OHM 57-52-11.
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